This code allows you to parametrize an airfoil shape using PARSEC method, then the code is using Genetic algorithm as an optimizer, you can view:
1- the airfoil before an after parameterization
2- Coefficient of lift change
the genetic algorithm is coded without using the embedded MATLAB optimizer for faster computation and simpler.
in case you need the GA in a generic format for any application to utilize it please comment and i will upload it.
Ziad Saad (2021). Optimization of an airfoil shape using Genetic algorithm(GA) (https://www.mathworks.com/matlabcentral/fileexchange/69095-optimization-of-an-airfoil-shape-using-genetic-algorithm-ga), MATLAB Central File Exchange. Retrieved .
I would be interested in seeing the GA in the generic format
Hello sir, How to get the initial parsec parameters?
Hello Sir, could you please upload the generic format for this code? thank you
Could you tell me how to select the rang of the initial value?
Hi Ziad, could you show how to get the Cd ?
kindly upload the generic format
I need GA in a generic format for airfoil otimization. kindly uplaoad it or provide the link
For the NACA-0012 airfoil I believe you should get a value of 0 for the coefficient of lift at 0 AOA. However, this is not the case. I'm not sure why -- does anyone have any ideas how to fix this?
I also need the GA in a generic format to find cl/cd ratio for an arifoil and cascade
I need the GA in a generic format so that I can utilize it by using CST method. I will be thankful to you for this.
I want to parametrize an asymmetrical airfoil shape using CST method, may I get the genetic algorithm code link with CST to get coefficient of lift. If you can please upload genetic algorithm code, I will try myself to link with CST.
Thank you so much in advance.
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